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contributor authorJ. H. Horlock
date accessioned2017-05-09T00:03:39Z
date available2017-05-09T00:03:39Z
date copyrightApril, 2000
date issued2000
identifier issn0889-504X
identifier otherJOTUEI-28676#218_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/124481
description abstractThe end-wall blockage in axial compressors has been the subject of several investigations over a period of many years. This paper reviews and compares various approaches to determining the blockage, particularly in the “repeating” stage, a stage deeply embedded in the compressor where an equilibrium state is reached, the flow through any one stage repeating in the next. These approaches include: (i) correlations of displacement thickness measured in compressor rigs; (ii) a relationship between outlet blockage and the clearance area, based both on an empirical development of a simple model of the flow through the clearance space and full CFD calculations of the flow; (iii) momentum analysis of the flow through the blockage region, developed from the boundary layer analyses of some years ago, but not now relying on boundary layer concepts. [S0889-504X(00)01502-6]
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Determination of End-Wall Blockage in Axial Compressors: A Comparison Between Various Approaches
typeJournal Paper
journal volume122
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.555452
journal fristpage218
journal lastpage224
identifier eissn1528-8900
keywordsPressure
keywordsMomentum
keywordsFlow (Dynamics)
keywordsCompressors
keywordsClearances (Engineering)
keywordsBoundary layers
keywordsRotors
keywordsBlades
keywordsThickness
keywordsStators
keywordsEquilibrium (Physics) AND Displacement
treeJournal of Turbomachinery:;2000:;volume( 122 ):;issue: 002
contenttypeFulltext


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